SKYCAR 200

Two passenger VTOL aircraft

Skycar 200

Originally conceived with military applications in mind, the general aviation Skycar 200 is a light weight, 2-passenger VTOL aircraft now targeted for local commuting markets. Capable of flight speeds of approximately 240 mph, the Skycar 200 design incorporates multiple redundancies and safety features, and its Flight Control System (FCS) virtually eliminates the complexities of flying. Even a novice operator can master the skills needed to maintain precise control over the aircraft. In the future, passengers will not be required to fly the aircraft, as it will be an autonomous craft utilizing onboard environment scanning and positioning systems, the highway-in-the-sky and automated air traffic control in order to fly between destinations and avoid airborne obstacles.

Skycar 200 Targeted Performance

VTOL Configuration        Two fixed thrust nacelles with one Rotapower engine and one electric motor per nacelle and a single lift duct with two electric motors
Seating        Tandem
Emergency Airframe Parachutes        Yes
Fuel Type        Ethanol
Dimensions (L x W x H) – Stowed footprint        14' x 8.5' x 6' - 1192
Gross Weight        1,320 lbs
Net Payload        400 lbs
Continuous Engine Power (Total)        170 hp
Electrical Motor Power (90 seconds)        85 hp per motor
Emergency Electrical Motor Power (30 seconds)        145 hp per motor
Component Articulation Required        Wing tips fold
Maximum Speed (Sea Level)        242 mph
Cruise Speed (Sea Level @ 65% power)        205 mph
Time – Parachute Safe (50 mph @ 200 ft)        11.3 seconds
Time to Transition (0-131 mph)        16.2 seconds
Maximum Endurance (Sea Level @ 131 mph)        3.7 hours
Rate of climb (sea level)        1,816 fpm
Time to climb (10,000 ft)        3.8 minutes
Roadability (On improved roads)        ~ 30 mph
Range with 2 passengers @ 122 mph (42 mpg)        434 miles
Fuel Consumption(Sea Level @ Cruise)        7.37 gallons per hour

SKYCAR 400

Four passenger VTOL aircraft

Skycar 400

The Skycar 400 is the 5th generation of VTOL aircraft developed by Dr. Paul Moller and is now at the “operational prototype” stage. The Skycar combines the high-speed capabilities of a fixedwing aircraft with the vertical take off and landing capabilities of a helicopter. Its ducted fans provide lift and propulsion without the dangerous exposed rotor blades and high maintenance costs of rotary-winged aircraft. The vehicle uses state-of-the-art fly-by-wire computer technology to monitor, control and maintain stability of the aircraft, while simultaneously making it simple and easy to operate.

Skycar 400 Targeted Performance

VTOL Configuration        Four fixed thrust nacelles with two counter-rotating Rotapower engines per nacelle
Passengers        2+2
Emergency Airframe Parachutes        Yes
Fuel Type        Ethanol
Noise Level at 500ft (Goal)        65 dBA
Dimensions (L x W x H)        21.5’ x 8.5’ x 7.5’        6.5m x 2.6m x 2.3m
Operational ceiling        36,000 ft        10973 m
Takeoff and landing area        35 ft dia        10.7 m
Max speed @sea-level        331 mph        533 km/h
Cruise Max speed @20,000 ft        308 mph        496 km/h
Rate of climb @sea-level        4,800 fpm        1,463 M/min
Endurance        5.9 hours
Disc loading        140 lb/ft2        684 kg/m2
Range @ 131 mph (21.3 mpg)        805 miles        1,213 km
Net payload        720 lbs        327 kg
Gross weight        2,400 lbs        1088 kg
Continuous Engine Power (Total)        720 hp        537 kW
Maximum Lift/Drag        12.5